Matches in DBpedia 2016-04 for { <http://citation.dbpedia.org/hash/0ac5fe0854c668d421c66ebded15298a7b5591ff2f87a338cc403bd989bb25e8> ?p ?o }
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- 0ac5fe0854c668d421c66ebded15298a7b5591ff2f87a338cc403bd989bb25e8 assign1 "EADS EUROP AERONAUTIC DEFENCE".
- 0ac5fe0854c668d421c66ebded15298a7b5591ff2f87a338cc403bd989bb25e8 country "FR".
- 0ac5fe0854c668d421c66ebded15298a7b5591ff2f87a338cc403bd989bb25e8 fdate "2011-02-10".
- 0ac5fe0854c668d421c66ebded15298a7b5591ff2f87a338cc403bd989bb25e8 invent1 "Aguilar, Michel".
- 0ac5fe0854c668d421c66ebded15298a7b5591ff2f87a338cc403bd989bb25e8 isCitedBy Xplorair.
- 0ac5fe0854c668d421c66ebded15298a7b5591ff2f87a338cc403bd989bb25e8 number "2971553".
- 0ac5fe0854c668d421c66ebded15298a7b5591ff2f87a338cc403bd989bb25e8 pridate "2011-02-10".
- 0ac5fe0854c668d421c66ebded15298a7b5591ff2f87a338cc403bd989bb25e8 pubdate "2012-08-17".
- 0ac5fe0854c668d421c66ebded15298a7b5591ff2f87a338cc403bd989bb25e8 status "application".
- 0ac5fe0854c668d421c66ebded15298a7b5591ff2f87a338cc403bd989bb25e8 title "Method for reducing noise of propulsion jet reactor of aircraft, involves ejecting shear flows at trailing edge of nacelles of reactor with ejection velocity in range between velocities of flows at inner and outer sides of nacelles".